姿态控制系统

基于Matlab的弹道导弹姿态控制系统设计与仿真软件研究

Research on Missile Attitude Control System Design and Simulation Software Based on Matlab

EMD在卫星姿态控制系统未知故障诊断中的应用

Novel fault diagnosis of satellite attitude control system based on EMD

垂直发射导弹Terminal滑模姿态控制系统设计

The Design of Terminal Sliding Control System for Vertical Launching Missile

运载火箭姿态控制系统的鲁棒H∞控制与设计

Robust H ∞ Control and design of Launch Vehicle Attitude Control Systems

FPGA在小卫星姿态控制系统中的应用

Application of FPGA in Control of Small Satellite Attitude

验证了本文设计的分数阶PID控制器针对无人机的姿态控制系统而言是有效的。

The comparations of simulation results , verified that the designed fractional order controllers for the attitude control system of UAV is effective .

姿态控制系统（CS）件负责维护航空器的姿态。

The Attitude Control System ( ACS ) software is responsible for maintaining the attitude of the spacecraft .

针对三轴稳定的质量矩导弹姿态控制系统，提出了一种基于遗传算法进行参数寻优的模糊PID控制方法。

A novel method of fuzzy proportional-integral-differential ( PID ) control by GA is designed for the attitude control system of three-axis-stable mass moment missile in this paper .

变质心BTT拦截导弹姿态控制系统设计

The Design of Attitude Control System of Moving Mass Actuated BTT Missile

本系统采用美国NationalInstrument公司的虚拟仪器开发软件LabWindows／CVI作为系统的软件开发工具，开发了模型姿态控制系统软件平台。

This system adopts LabWindows / CVI , the American National Instrument corporation 's virtual instrument developing software , develop control system software platform of model attitude .

另一方面，文中建立了运载火箭姿态控制系统仿真模型，研究在MATLAB环境下对一类复杂的时变系统仿真的问题。

The other builds the simulation model for the rocket control system based on MATLAB , settles the problems which occur when simulating complex and time-varying systems under MATLAB / SIMULINK environment .

基于STK的小卫星零动量姿态控制系统仿真研究

Research on the Simulation of Small Satellite 's Zero-Momentum Attitude Control System Based on STK

为提高传统卫星姿态控制系统精度，提出了一种基于小脑模型（CMAC）神经网络的比例-积分-微分（PID）的复合控制器。

To improve the control accuracy of traditional attitude controller for satellite , a CMAC neural network PID hybrid attitude controller was put forward in this paper .

基于Ackermann规则的离散全程灰色滑模控制在数字导弹姿态控制系统中的应用

Application of Ackermann Formula Based Discrete Grey Sliding Mode Control in Digital Missile Attitude Control System

由于导弹姿态控制系统模型的精确性有限，常规Kalman滤波方法因其鲁棒性差很难检测故障，这种方法能有效检测故障。

Because the accuracy of missile attitude control system model is limited , it is difficult to detect fault for the traditional Kalman filter owing to its weak robustness . The improved algorithm can detect faults effectively .

在零动量的假设下，利用Backstepping滑模控制方法，为基于（w，z）参数描述的欠驱动姿态控制系统设计了一个新型的姿态控制器。

A new controller is designed by using the Backstepping sliding mode control method for the under-actuated systems described by ( w , z ) parameter , under the assumption of zero momentum for the spacecraft .

利用MSCADAMS中用户自定义子程序方法建立卫星姿态控制系统的模型，对卫星附件在轨展开过程进行卫星姿态动力学仿真分析。

This satellite attitude control system model is established by using MSC Adams user subroutine . The simulation analysis of the satellite attitude dynamics during the process of appurtenances deployment in the space is discussed .

介绍了利用NI公司的高速定时器/计数器以及含步进电机的CCD线阵列式位置传感器支架来实现的磁悬挂天平的俯仰和平动姿态控制系统。

By using the high speed timer / counter of NI company , the pitching and flat pose control system of MSBS was introduced in this paper . The bracket of this system contained step motion of CCD line array situation sensor .

利用H∞控制理论对船舶减摇鳍横摇姿态控制系统进行了混合灵敏度设计，并针对船舶减摇鳍系统的特殊性，解决了H∞控制器设计中与该系统不匹配的有关问题。

By using the H ∞ control theory , a mixture sensibility design was made for a fin stabilizer system . The mismatch problem in the design of H ∞ controller associated with the system was solved in accordance with the features of the ship roll damping .

这就对EKV的导引律设计和姿态控制系统提出了很高的要求。

This entails a high requirement for the design of the Guidance Law and the control of the posture .

然后分析和研究小卫星零动量姿态控制系统的设计思想，同时建立小卫星的三维模型，并在STK中进行仿真应用；

Secondly , the design processes of small satellite 's attitude control system and its three dimensional model is deeply researched and realized in the STK 's scenario .

ASV再入大气层的飞行环境变化剧烈、干扰大，因而其姿态控制系统的设计是一项非常前沿的研究课题。

For the varieties of the aerosphere and the large disturbances , the design of attitude control system of ASV is a very difficult problem during the re-entry .

本文对RBV再入段姿态控制系统的设计理论和方法进行研究，采用鲁棒控制中的μ综合理论与增益调度控制结合的方式设计控制器。

This thesis researched the attitude control system of RBV in reentry phase , using a method , which integrates the μ - synthesis in robust control theory with the gain schedule control method , to design the controller .

本篇论文研究提出了一种运载火箭姿态控制系统的故障分析法，称为故障-功能分析法（简称为F-FAM）。

This paper proposes a failure diagnosis method , called failure-function analysis method ( F-FAM ), for an attitude control system in a carrier rocket .

负温度系数（NTC）热敏电阻型是国内外地球卫星姿态控制系统用主要红外探测器类型之一，也是该系统的核心元器件，其性能对整个卫星姿态控制系统影响重大。

At home and abroad Negative temperature coefficient ( NTC ) type thermistor Earth satellite attitude control systems is one of the main types of infrared detectors , Is also the core of the system components , its performance has major impact for the satellite attitude control system .

另外，EKV在末段拦截过程中，其姿控推力是由脉冲固体火箭发动机组提供，在设计姿态控制系统时，应充分考虑这种推力形式带来的影响。

In addition , while EKV intercepting of the latter end , the attitude control thrust is provided by the solid rocket motors . When designing the posture control systems , one should fully consider the impact brought by this thrust .

上述方法已经用于以实际的卫星姿态控制系统为背景的实时故障诊断专家系统（SCRDES），它是ES技术在实时监测系统中应用的一个新探索。

A kind of feasible structure of hardware and software for knowledge processing is given , the above-mentioned methods have been applied to the Real-time Diagnosis Expert System for recoverable Satellite attitude Control system ( SCRDES ), which is a new probing into ES in real-time monitor filed .

本文结合国家863科研计划项目深空探测自主技术与仿真演示系统（2004AA735080），对深空探测器姿态控制系统设计方法进行了研究。

For deep space explorer , the attitude control system design methods were studied in this dissertation , which is funded by the National 863 Plan ( 2004AA735080 ), Autonomy Technology and Simulation Demonstration System for Deep Exploration .

导弹姿态控制系统最佳测试点的选取

Determination of the Optimal Testing Points for Missile Attitude Control System

质量矩拦截弹的模糊滑模姿态控制系统设计

Fuzzy Sliding Mode Attitude Control Approach to Mass Moment Interception Missile